View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 23432U 26159.18770970 +.00000000 +00000-0 +68871-4 0 00003
2 23432 74.0328 61.0212 0005902 205.9376 268.0031 14.34462304 01
| Epoch (UTC): | 08 June 2026 04:30:18 |
| Eccentricity: | 0.0005902 |
| inclination: | 74.0328° |
| perigee height: | 773 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 61.0212° |
| argument of perigee: | 205.9376° |
| revolutions per day: | 14.34462304 |
| mean anomaly at epoch: | 268.0031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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